The design of high attack-angle flying missile control system based on feedback Linearization

被引：0
|
作者：
Yan-Ke, Xu [1 ]
Xiao-Geng, Liang [2 ]
Xiao-Hong, Jia [3 ]
机构：
[1] Department of Automatic Control, Northwestern Polytechnical University, Xi'an, China
[2] China Airborne Missile Academy, Luoyang, China
[3] China Airborne Missile Academy, Luoyang, China
来源：
Journal of Convergence Information Technology | 2012年 / 7卷 / 03期
关键词：
Equations of motion - Feedback linearization - Missiles - Variable structure control;
D O I：
10.4156/jcit.vol7.issue3.18
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：155 / 163
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